SBIR/STTR Research Award

Development of a Novel Control Surface and Actuation System for High Lift-to-Drag Vehicles Using the Rapid Hypersonic Yaw Maneuver Evaluation Framework (RHYME)

Award identifier 4af2dbfd1f663315fdae351be6f31dba9f1a6b2cfc565416105be6a1bfdfe92eAwarding agency Department of Defense · Missile Defense Agency

Award amount

$1,469,708

Program and phase

STTR · Phase II

Award year

2025

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Award details

Awarding agency
Department of Defense
Branch
Missile Defense Agency
Recipient company
CFD Research Corporation
Proposal award date
2025-02-26
Contract end date
2027-02-25
UEI
V3KCP1HNFM33
Solicitation number
23.B
Topic code
MDA23-T004

Research abstract

In this Phase II effort, and in collaboration with the vehicle prime contractor, we propose to design, build, and plan for integration of advanced control surfaces for high lift-to-drag (L/D) hypersonic vehicles to enable fast yaw maneuvers. To meet this objective, we will initially focus on development and validation of a modeling and simulation framework, called Rapid Hypersonic Yaw Maneuver Evaluation (RHYME) for the assessment and optimization of these innovative aerodynamic hypersonic control concepts toward their ability to reduce the time constants of yaw maneuvers. Within this framework, initial candidate designs are defined, aerodynamic databases are generated, and the maneuverability efficiencies of these concepts are evaluated by assessing the aerodynamic performance through trajectory analysis. In Phase I, the principal workflow was established, a preliminary experimental setup for hypersonic testing was defined, and a preliminary optimization study was performed. Also, an initial integration concept for the down-selected designs was presented. Efforts in Phase II will include full six degrees of freedom (6DoF) guidance navigation and control (GNC) simulations coupled with CFD Research’s in-house Multi-objective Surrogate-assisted Evolutionary Algorithms for Guided Weapon Design (MEADOW). Optimization objectives in Phase II include minimizing the maneuver time, drag, and volume/mass of the additional control surfaces while maximizing the available kinetic energy and range of the vehicle. The aerodynamic predictions of the framework will be anchored and validated by hypersonic high-enthalpy experiments also executed in Phase II. Testing will occur across a range of Mach numbers and altitudes, with the ability to assess high-enthalpy effects on flow transition and separation in the vicinity of the control surfaces. Starting in Phase II and continuing into beyond-Phase II and Phase III efforts, we will work on maturing the design to enable integration into a full guidance, navigation, and control system solution, also in collaboration with the vehicle prime contractor. Approved for Public Release | 25-MDA-12052 (27 Mar 25)

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

947 SBIR/STTR records share this UEI (1987–2026). Reported award amounts total $350,893,199. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Health and Human Services, National Science Foundation, Department of Commerce, Department of Energy

Agency intelligence

Department of Defense

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